Preliminary Investigation Into the Effects of Cross-Flow on Low Reynolds Number Transition-Reference-Cited by-同舟云学术

Preliminary Investigation Into the Effects of Cross-Flow on Low Reynolds Number Transition

Published:2011-06-14 Issue: Volume: Page:
ISSN:
Container-title:20th AIAA Computational Fluid Dynamics Conference
language:
Short-container-title:

Author:

Uranga Alejandra¹,Persson Per-Olof²,Drela Mark¹,Peraire Jaime¹

Affiliation:

1. Massachusetts Institute of Technology

2. University of California, Berkeley

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3558

Reference20 articles.

1. Implicit Large Eddy Simulation of Transitional Flows Over Airfoils and Wings

2. Implicit Large Eddy Simulation of transition to turbulence at low Reynolds numbers using a Discontinuous Galerkin method

3. 3Uranga, A., Investigation of transition to turbulence at low Reynolds numbers using Implicit Large Eddy Simulations with a Discontinuous Galerkin method, Ph.D. thesis,Massachusetts Institute of Technology, Cambridge, MA, 2011.

4. Stability of Three-Dimensional Boundary Layers

5. Linear Stability Theory Applied to Boundary Layers

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Effects of Sweep Angle in Aeroelastic Response of Wings Made of Isotropic and Fiber Reinforced Composite Materials;2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2018-01-07

2. Boundary Layer Ingestion Benefit of the D8 Transport Aircraft;AIAA Journal;2017-11

3. Numerical study of streamwise and cross flow in the presence of heat and mass transfer;The European Physical Journal Plus;2017-05

4. Design Practice for the Horizontal Fin of a Single Screw-Twin Rudder System;Journal of The Japan Institute of Marine Engineering;2014